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Closed Loop Blade Tone Control in Axial Turbomachines by Flow Induced Secondary Sources in a Blade Tip Regime

Lemke, O. and Neise, W. and Enghardt, L. and King, R. and Muminovic, R. and Möser, M. (2010) Closed Loop Blade Tone Control in Axial Turbomachines by Flow Induced Secondary Sources in a Blade Tip Regime. In: Active Flow Control II (Vol. 108). Springer. Active Flow Control II Conference, 26.-28. Mai 2010, Berlin, Deuschland. ISBN 978-3-642-11734-3

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Item URL in elib:https://elib.dlr.de/68786/
Document Type:Conference or Workshop Item (Paper)
Title:Closed Loop Blade Tone Control in Axial Turbomachines by Flow Induced Secondary Sources in a Blade Tip Regime
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lemke, O.Institut für Strömungstechnik und Technische Akustik, TU BerlinUNSPECIFIED
Neise, W.UNSPECIFIEDUNSPECIFIED
Enghardt, L.UNSPECIFIEDUNSPECIFIED
King, R.Institut für Prozess- und Verfahrenstechnik, TU BerlinUNSPECIFIED
Muminovic, R.Institut für Prozess- und Verfahrenstechnik, TU BerlinUNSPECIFIED
Möser, M.Institut für Strömungstechnik und Technische Akustik, TU BerlinUNSPECIFIED
Date:2010
Journal or Publication Title:Active Flow Control II
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmail
King, R.Institut für Prozess- und Verfahrenstechnik, TU Berlin
Publisher:Springer
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISBN:978-3-642-11734-3
Status:Published
Keywords:blade tone control, axial turbomachines,
Event Title:Active Flow Control II Conference
Event Location:Berlin, Deuschland
Event Type:international Conference
Event Dates:26.-28. Mai 2010
Organizer:Collaborative Research Center on Flow Control in Berlin
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies (old)
Location: Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Kaur, Balbir
Deposited On:02 Feb 2011 11:33
Last Modified:02 Feb 2011 11:33

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